High-Speed Local Particle Injection for Particle Image Velocimetry
Author:
Affiliation:
1. Arnold Engineering Development Complex, Arnold Air Force Base, Tennessee 37389
Funder
Air Force Office of Scientific Research
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.J057654
Reference44 articles.
1. The Hypervelocity Wind Tunnel No. 9; Continued Excellence Through Improvement and Modernization
2. Investigation by Particle Image Velocimetry Measurements of Oblique Shock Reflection with Separation
3. The Effect of Particle Lag on Supersonic Turbulent Boundary Layer Statistics
4. Nanostructured tracers for laser-based diagnostics in high-speed flows
5. Experimental Investigation of Hypersonic Turbulent Boundary Layer
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